CHI06LA207

NTSB accident investigation · Schlei Avid Flyer Speed Win · Fergus Falls, MN · July 21, 2006

Accident · Serious injuriesLimited investigationFinal report
Date
July 20, 2006, 20:05 local (Jul 21, 2006, 01:05 UTC)
Place
Fergus Falls, MN
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N507SSchlei Avid Flyer Speed Win
Weather
Visual (VMC) · Night
Status
Completed · report November 29, 2007
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20060720015089A
Case key
64354

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

the fractured aileron bell crank and elevator clevis rod end.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionCruise
Flt control syst,elevator control - fracturedCause
In flight collision with terrain/waterEmergency landing
Terrain condition - ground

Analysis

An experimental amateur-built airplane impacted terrain during an emergency landing following a loss of control during cruise flight. Examination of the flight control system revealed a broken front aileron bell crank and a broken elevator clevis rod, which had a fracture that was more than half rusted.

Factual narrative

On July 20, 2006, at 2006 central daylight time, an experimental amateur-built Schlei Avid Flyer Speed Wing, N507S, owned and piloted by a private pilot, received substantial damage on impact with terrain during an emergency landing. The pilot reported a loss of control. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 personal flight was not operating on a flight plan. The pilot received serious injuries. The flight departed from Henning, Minnesota, and was returning to Fergus Falls, Minnesota.

The pilot stated that after he descended from a cruise altitude of 4,000 feet and "shortly" after leveling off at 3,000 feet, he felt the airplane "kind of shake." Following the shake, the airplane pitched down with a "slight" left bank. He thought he was in a spin so he reduced engine power to idle and applied right rudder but there was no effect on airplane control. Out of "desperation," he began to move the control stick "all over," looking for anything that would return control. He moved the control stick as far aft as and to the right as possible. The airplane began to level off. Hoping to level the attitude some more, he tried moving the control stick again but the airplane began "going down again." He then moved the control stick to its previous position but did not remember if it had an effect on airplane attitude. He knew that he was going to "crash," so he turned the fuel off and was going to turn the master switch off but did not remember if he did.

Examination of the flight control system by the Federal Aviation Administration revealed a broken front aileron bell crank (part identification F-5). Additionally, there was a broken elevator clevis rod end (part identification F-43), which had a fracture that was more than half rusted.

Aircraft

Registration
N507S
Reported as
Schlei Avid Flyer Speed Win
Category
Airplane, amateur-built
Serial number
507
Airframe hours
247.3
Engine
Rotax 582UL, 65 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Pilot
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · October 1, 2005 · 8 hours before
Departed
Henning, MN
Destination
FFM · Fergus Falls, MN
Airport
FFM · Fergus Falls Muni-Einar Mickel

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
65
Injuries
Serious
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3
Last flight review
July 1, 2006
Seat
Left
Flight hours
200 total · 63 in this make and model · 115 as pilot in command

Weather

Conditions
Visual (VMC) · Night
Wind
360° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 61 °F
Altimeter
30.14 inHg
Observed at
FFM, 8 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.